03.1 - Aerodynamics – CFD Methods and Validation
A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES
E. Levati¹, C. Pasquali¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy
This work deals with the derivation of a novel boundary integral formulation for potential flows useful for the aerodynamic and aeroacoustic analysis of deformable bodies in compressible flows. Current developments in aviation design and the increased demand for innovative aircraft, with unconventional geometry, require more reliable and efficient tools for aerodynamic and aeroacoustic analyses.